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NASA/LANGLEY LS(1)-0413 (GA(W)-2) AIRFOIL (ls413-il)

NASA/LANGLEY LS(1)-0413 (GA(W)-2) AIRFOIL - NASA/Langley LS(1)-0413 (GA(W)-2) general aviation airfoil


Airfoil ls413-il
Details Dat file Parser  
(ls413-il) NASA/LANGLEY LS(1)-0413 (GA(W)-2) AIRFOIL
NASA/Langley LS(1)-0413 (GA(W)-2) general aviation airfoil
Max thickness 12.9% at 37.5% chord.
Max camber 2.4% at 65% chord
Source UIUC Airfoil Coordinates Database
Source dat file
The dat file is in Lednicer format
 NASA/LANGLEY LS(1)-0413 (GA(W)-2) AIRFOIL
45.        45.
 
 0.00000   0.00000
  .00200    .01040
  .00500    .01590
  .01250    .02420
  .02500    .03320
  .03750    .03970
  .05000    .04480
  .07500    .05260
  .10000    .05860
  .12500    .06350
  .15000    .06750
  .17500    .07100
  .20000    .07400
  .22500    .07650
  .25000    .07860
  .27500    .08030
  .30000    .08180
  .32500    .08300
  .35000    .08380
  .37500    .08430
  .40000    .08460
  .42500    .08460
  .45000    .08440
  .47500    .08380
  .50000    .08290
  .52500    .08170
  .55000    .08020
  .57500    .07830
  .60000    .07610
  .62500    .07330
  .65000    .07020
  .67500    .06670
  .70000    .06290
  .72500    .05870
  .75000    .05420
  .77500    .04950
  .80000    .04450
  .82500    .03930
  .85000    .03400
  .87500    .02840
  .90000    .02270
  .92500    .01690
  .95000    .01100
  .97500    .00480
 1.00000   -.00160
 
 0.00000   0.00000
  .00200   -.00500
  .00500   -.00940
  .01250   -.01450
  .02500   -.01910
  .03750   -.02230
  .05000   -.02500
  .07500   -.02940
  .10000   -.03280
  .12500   -.03560
  .15000   -.03790
  .17500   -.03980
  .20000   -.04140
  .22500   -.04270
  .25000   -.04370
  .27500   -.04430
  .30000   -.04480
  .32500   -.04510
  .35000   -.04520
  .37500   -.04500
  .40000   -.04470
  .42500   -.04420
  .45000   -.04350
  .47500   -.04260
  .50000   -.04140
  .52500   -.03990
  .55000   -.03810
  .57500   -.03590
  .60000   -.03330
  .62500   -.03050
  .65000   -.02740
  .67500   -.02420
  .70000   -.02100
  .72500   -.01770
  .75000   -.01440
  .77500   -.01130
  .80000   -.00830
  .82500   -.00570
  .85000   -.00350
  .87500   -.00180
  .90000   -.00080
  .92500   -.00060
  .95000   -.00130
  .97500   -.00340
 1.00000   -.00710
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Lednicer format dat file
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Polars for NASA/LANGLEY LS(1)-0413 (GA(W)-2) AIRFOIL (ls413-il)

PlotAirfoilReynolds #NcritMax Cl/CdDescriptionSource 
   ls413-il50,000935.9 at α=6°Mach=0 Ncrit=9Xfoil predictionDetails
   ls413-il50,000533.8 at α=5.75°Mach=0 Ncrit=5Xfoil predictionDetails
   ls413-il100,000953 at α=5.25°Mach=0 Ncrit=9Xfoil predictionDetails
   ls413-il100,000548.8 at α=4.5°Mach=0 Ncrit=5Xfoil predictionDetails
   ls413-il200,000969.5 at α=4.25°Mach=0 Ncrit=9Xfoil predictionDetails
   ls413-il200,000565.7 at α=3°Mach=0 Ncrit=5Xfoil predictionDetails
   ls413-il500,000996.2 at α=3°Mach=0 Ncrit=9Xfoil predictionDetails
   ls413-il500,000582.5 at α=1.5°Mach=0 Ncrit=5Xfoil predictionDetails
   ls413-il1,000,0009112.4 at α=2°Mach=0 Ncrit=9Xfoil predictionDetails
   ls413-il1,000,000586.4 at α=0.5°Mach=0 Ncrit=5Xfoil predictionDetails
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